Volume 14, Issue 4 (December 1992)

    Prediction of Matrix Fatigue Crack Initiation in Notched SCS-6/Ti-15-3 Metal Matrix Composites

    CODEN: CTROAD

      Format Pages Price  
    PDF Version 4 $25   ADD TO CART


    Abstract

    Several lay-ups of SCS-6/Ti-15-3 metal matrix composites were tested in either a center hole or a double-edge-notched geometry. At different cyclic stress levels, the number of cycles required to initiate a matrix fatigue crack at the notch was recorded. A strain-life fatigue curve was developed for the Ti-15-3 matrix material. A strain-life fatigue analysis method was developed that incorporates a modified Smith, Watson, and Topper effective strain parameter to account for local stress concentration at the notch tip and thermal residual stresses in the matrix material. This analysis method was used to predict the number of cycles required for matrix crack initiation at the notches. The predictions were in good agreement with the experimental data.


    Author Information:

    Hillberry, BM
    Professor, School of Mechanical Engineering, Purdue University, West Lafayette, IN

    Steven Johnson, W
    Senior research scientist, NASA Langley Research Center, Hampton, VA


    Stock #: CTR10101J

    ISSN: 0884-6804

    DOI: 10.1520/CTR10101J

    ASTM International is a member of CrossRef.

    Author
    Title Prediction of Matrix Fatigue Crack Initiation in Notched SCS-6/Ti-15-3 Metal Matrix Composites
    Symposium , 0000-00-00
    Committee D30